US11131010B2ActiveUtilityA1
Titanium alloy and method of manufacturing material for timepiece exterior part
Est. expiryApr 14, 2036(~9.8 yrs left)· nominal 20-yr term from priority
C22F 1/00C22F 1/183C22F 1/18C22C 14/00
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Claims
Abstract
A titanium alloy of the present invention includes aluminum at a ratio of 28.0 at % or more and 38.0 at % or less, iron at a ratio of 2.0 at % or more and 6.0 at % or less, and titanium and inevitable impurities as the balance or includes aluminum at a ratio of 28.0 at % or more and 38.0 at % or less, manganese at a ratio of 4.0 at % or more and 8.0 at % or less, and titanium and inevitable impurities as the balance. Further, the titanium alloy of the present invention may include silicon at a ratio of 0.3 at % or more and 1.5 at % or less.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1. A method of manufacturing a material for a timepiece exterior part, the method comprising:
a first heat treatment step of heating a casted titanium alloy at a temperature in a range of 1200° C. or higher and 1300° C. or lower in a furnace, the titanium alloy being cooled down at a room temperature thereafter by taking out from the furnace;
a forging step of forging the titanium alloy after the first heat treatment step at a room temperature in an atmosphere, or a hot working step of performing hot working on the titanium alloy after the first heat treatment step at a room temperature in an atmosphere; and
a second heat treatment step of heat-treating the titanium alloy at a temperature in a range of 1200° C. or higher and 1300° C. or lower after the forging step or the hot working step, the titanium alloy being cooled down to a room temperature thereafter to form a timepiece exterior part,
wherein the titanium alloy consists of:
aluminum at a ratio of 28.0 at % or more and 38.0 at % or less;
iron at a ratio of 2.0 at % or more and 6.0 at % or less; and
titanium and inevitable impurities as the balance,
wherein after the second heat treatment step, the titanium alloy is cooled at a cooling rate equal to or higher than that of air cooling,
the method is free of a surface hardening treatment step, and
the timepiece exterior part has a Vickers hardness of HV 600 or more.
2. A method of manufacturing a material for a timepiece exterior part, the method comprising:
a first heat treatment step of heating a casted titanium alloy at a temperature in a range of 1200° C. or higher and 1300° C. or lower in a furnace, the titanium alloy being cooled down at a room temperature thereafter by taking out from the furnace;
a forging step of forging the titanium alloy after the first heat treatment step at a room temperature in an atmosphere, or a hot working step of performing hot working on the titanium alloy after the first heat treatment step at a room temperature in an atmosphere; and
a second heat treatment step of heat-treating the titanium alloy at a temperature in a range of 1200° C. or higher and 1300° C. or lower after the forging step or the hot working step, the titanium alloy being cooled down to a room temperature thereafter to form a timepiece exterior part,
wherein the titanium alloy consists of:
aluminum at a ratio of 28.0 at % or more and 38.0 at % or less;
iron at a ratio of 2.0 at % or more and 6.0 at % or less;
silicon at a ratio of 0.3 at % or more and 1.5 at % or less and
titanium and inevitable impurities as the balance,
wherein after the second heat treatment step, the titanium alloy is cooled at a cooling rate equal to or higher than that of air cooling, and
the method is free of a surface hardening treatment step, and
the timepiece exterior part has a Vickers hardness of HV 600 or more.
3. The method according to claim 1 , wherein the titanium alloy consisting the timepiece exterior part is in a B2 phase of an intermetallic compound phase.
4. The method according to claim 2 , wherein the titanium alloy consisting the timepiece exterior part is in a B2 phase of an intermetallic compound phase.Cited by (0)
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